Long Hu, Hu Yaming, Liu Jiaxin, Wang Wei, Liao Guanglan, Yuen Anthony Chun Yin, Yeoh Guan-Heng, Hu Yuan, Shi Tielin
State key Laboratory of Intelligent Manufacturing Equipment and Technology, School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, P. R. China.
School of Mechanical and Manufacturing Engineering, University of New South Wales, Sydney 2052, Australia.
ACS Appl Mater Interfaces. 2024 Sep 25;16(38):51421-51432. doi: 10.1021/acsami.4c09506. Epub 2024 Sep 16.
With rapid advancements in aerospace and supersonic aircraft technology, there is a growing demand for multifunctional thermal protective materials. Aerogels, known for their low density and high porosity, have garnered significant attention in this regard. However, developing a lightweight multifunctional aerogel that combines exceptional thermal and mechanical properties through a straightforward and time-efficient method remains a significant challenge. Herein, a facile and universal approach is developed for the preparation of Kevlar/hexagonal boron nitride (h-BN) aerogels, in which a spin-assisted method is applied to create robust microribbons and further accelerate solvent displacement. The resulting microribbon scaffold, with its entangled nanofiber-nanosheet morphologies, exhibits sufficient strength to prevent volume shrinkage during drying, thereby allowing precise control over aerogel density. The porous hybrid aerogels, featuring controllable geometric characteristics and tailored densities ranging from 6.9 to 100 mg cm, can be successfully fabricated. These aerogels exhibit excellent thermal insulation properties, and the thermal conductivities of the as-prepared KB aerogels have a wide distribution in the range of 0.0269-0.0450 W m k. The thermal stability of the hybrid aerogels is enhanced to 566 °C. Moreover, the resulting hybrid aerogels exhibit an ultrahigh bearing ratio, supporting more than 2000 times their own weight while maintaining stable structural integrity. These aerogels also demonstrate high compressive strength, hydrophobicity, and excellent sorption performance for various oils and solvents. Additionally, the oil-saturated aerogels can be easily recovered through heat treatment or combustion in air. The features endow hybrid Kevlar/h-BN aerogels with significant potential for applications in thermal management, environmental protection, and neutron protection.
随着航空航天和超音速飞机技术的飞速发展,对多功能热防护材料的需求日益增长。气凝胶以其低密度和高孔隙率而闻名,在这方面受到了广泛关注。然而,通过一种简单且高效的方法开发出一种兼具优异热性能和机械性能的轻质多功能气凝胶仍然是一项重大挑战。在此,我们开发了一种简便通用的方法来制备凯夫拉尔/六方氮化硼(h-BN)气凝胶,其中采用了旋转辅助方法来形成坚固的微带,并进一步加速溶剂置换。所得的微带支架具有缠结的纳米纤维-纳米片形态,展现出足够的强度以防止干燥过程中的体积收缩,从而能够精确控制气凝胶的密度。可以成功制备出具有可控几何特征且密度在6.9至100 mg/cm范围内的多孔混合气凝胶。这些气凝胶具有优异的隔热性能,所制备的KB气凝胶的热导率在0.0269 - 0.0450 W/(m·K)范围内广泛分布。混合气凝胶的热稳定性提高到了566℃。此外,所得的混合气凝胶表现出超高的承载比,能支撑超过自身重量2000倍的重量,同时保持稳定的结构完整性。这些气凝胶还具有高抗压强度、疏水性以及对各种油类和溶剂的优异吸附性能。此外,油饱和的气凝胶可以通过热处理或在空气中燃烧轻松回收。这些特性赋予了混合凯夫拉尔/h-BN气凝胶在热管理、环境保护和中子防护方面的巨大应用潜力。